<?xml version="1.0" encoding="UTF-8"?>
<!DOCTYPE ep-patent-document PUBLIC "-//EPO//EP PATENT DOCUMENT 1.1//EN" "ep-patent-document-v1-1.dtd">
<ep-patent-document id="EP99963147B1" file="EP99963147NWB1.xml" lang="en" country="EP" doc-number="1017935" kind="B1" date-publ="20031112" status="n" dtd-version="ep-patent-document-v1-1">
<SDOBI lang="en"><B000><eptags><B001EP>......DE....FRGB..IT............................................................</B001EP><B003EP>*</B003EP><B005EP>J</B005EP><B007EP>DIM350 (Ver 2.1 Jan 2001)
 2100000/0</B007EP></eptags></B000><B100><B110>1017935</B110><B120><B121>EUROPEAN PATENT SPECIFICATION</B121></B120><B130>B1</B130><B140><date>20031112</date></B140><B190>EP</B190></B100><B200><B210>99963147.6</B210><B220><date>19990111</date></B220><B240><B241><date>20000331</date></B241><B242><date>20020820</date></B242></B240><B250>en</B250><B251EP>en</B251EP><B260>en</B260></B200><B300><B310>98000077</B310><B320><date>19980728</date></B320><B330><ctry>ID</ctry></B330></B300><B400><B405><date>20031112</date><bnum>200346</bnum></B405><B430><date>20000712</date><bnum>200028</bnum></B430><B450><date>20031112</date><bnum>200346</bnum></B450></B400><B500><B510><B516>7</B516><B511> 7F 02M  29/06   A</B511></B510><B540><B541>de</B541><B542>LUFTDRALLERZEUGUNGSVORRICHTUNG AM LUFTEINLASSYSTEM EINER BRENNKRAFTMASCHINE</B542><B541>en</B541><B542>AIR FLOW-TWISTING DEVICE ON AN AIR INLET SYSTEM OF INTERNAL COMBUSTION ENGINE</B542><B541>fr</B541><B542>DISPOSITIF A ECOULEMENT D'AIR HELICOIDAL REPOSANT SUR UN SYSTEME D'ADMISSION D'AIR D'UN MOTEUR A COMBUSTION INTERNE</B542></B540><B560><B561><text>FR-A- 362 694</text></B561><B561><text>FR-A- 728 486</text></B561><B561><text>GB-A- 399 679</text></B561><B561><text>GB-A- 2 275 081</text></B561><B561><text>US-A- 1 606 916</text></B561><B561><text>US-A- 4 478 198</text></B561></B560></B500><B700><B720><B721><snm>Wijaya, Heru Prasanta</snm><adr><str>Graha Famili D.183, PR. Kali Kendal</str><city>Surabaya 60226</city><ctry>ID</ctry></adr></B721></B720><B730><B731><snm>Wijaya, Heru Prasanta</snm><iid>02658200</iid><irf>WYA-P1EP(WO)</irf><adr><str>Graha Famili D.183, PR. Kali Kendal</str><city>Surabaya 60226</city><ctry>ID</ctry></adr></B731></B730><B740><B741><snm>RACKETTE Partnerschaft Patentanwälte</snm><iid>00101482</iid><adr><str>Postfach 13 10</str><city>79013 Freiburg</city><ctry>DE</ctry></adr></B741></B740></B700><B800><B840><ctry>DE</ctry><ctry>FR</ctry><ctry>GB</ctry><ctry>IT</ctry></B840><B860><B861><dnum><anum>IB9900029</anum></dnum><date>19990111</date></B861><B862>en</B862></B860><B870><B871><dnum><pnum>WO00006889</pnum></dnum><date>20000210</date><bnum>200006</bnum></B871></B870></B800></SDOBI><!-- EPO <DP n="1"> -->
<description id="desc" lang="en">
<heading id="h0001"><u>Technical Field of Invention</u></heading>
<p id="p0001" num="0001">The present invention relates to a device called air flow-twisting device on an air inlet system of internal combustion engine, particularly an air flow-twisting device installed after air filter as an accessories means of air inlet system.</p>
<heading id="h0002"><u>Background of Invention</u></heading>
<p id="p0002" num="0002">Nowadays, the internal combustion engine is enforced to have high performance engine. One of the important aspect in the internal combustion engine is a perfect mixture of air and fuel, i.e., a homogenously and proportionally mixed air and fuel. Clean air that can be perfectly mixtured with fuel is a must.</p>
<p id="p0003" num="0003">A variety of air inlet system have been created for a better combustion effect such as the shapes or other supporting elements. However, such improved shapes and supporting elements which are present, have limited function in increasing speed and cleaness of air inlet system that will flow into mixture chamber of air and fuel after passing air filter to achieve a complete combustion level and a low waste gas emission.</p>
<p id="p0004" num="0004">In order to improve combustion process of an internal combustion engine, it is required to design a device or supporting elements in the air inlet system. Such design can increase the mixture of air and fuel flowing uniformly into internal combustion engine chamber.</p>
<heading id="h0003"><u>Short Description of Invention</u></heading>
<p id="p0005" num="0005">The present invention is made due to the problems presently exist in the prior invention. Therefore, object of the present invention is to prepare an air flow-twisting device installed in the air inlet system between air filter<!-- EPO <DP n="2"> --> and combustion chamber wherein the device will cause the perfect stirred effect and mixture of air and fuel in combustion chamber. The effect thus improves the combustion process and engine performance.</p>
<heading id="h0004"><u>Brief Description of the Drawing</u></heading>
<p id="p0006" num="0006">The objects and features of the invention will be made apparent as the detailed of the description progresses refers to the enclosed drawings, wherein:
<ul id="ul0001" list-style="none" compact="compact">
<li>Figure 1a is a two-dimensional cross section view of basic structure of air flow-twisting device installed at rubber tube for internal combustion engine according to the invention.</li>
<li>Figure 1b is three-dimensional cross section view of basic structure of air flow twisting device installed at rubber tube for internal combustion engine.</li>
<li>Figure 2 is a schematic diagram indicating position of air flow twisting device in the air inlet system of internal combustion engine.</li>
</ul></p>
<heading id="h0005"><u>Detailed Description of Invention</u></heading>
<p id="p0007" num="0007">Referring to Figures 1a and 1b, it is shown a basic construction of air flow twisting device (1) for internal combustion engine installed at rubber tube (2) of air inlet system. Air flow twisting device with a circumference tube shape having wall thickness corresponds to that wall thickness of rubber tube (2), and both end are cylindrical flange (3). About two-third of inner hollow length (a) from the body of air flow twisting device (4), is formed with twisted extending grooves (4) between the gap and distance of each uniform groove. One-third of the length of air flow twisting device body (b) is made regular inner circumferential hollow and with cylindrical flange end (3). Cylindrical flange end (3) of air flow twisting device (1) is connected into intake manifold (not shown) at the internal combustion engine with injection system or into intake carburator (not shown) when engine uses carburator. Air flow twisting device (1) can be made from various<!-- EPO <DP n="3"> --> material such as metal, polymer or ceramic.</p>
<p id="p0008" num="0008">Figure 2 illustrates a schematic diagram which indicates position of air flow twisting device in air inlet system of the internal combustion engine. Air flow twisting device (1) is substantially placed between air filter (5) and internal combustion engine (6). Air flow twisting device (1) can be installed in the air inlet system of internal combustion engine without changing basic contruction of the engine. Air flowing in after the air filter (5) is flown-out through air flow twisting device (1). When passing inner hollow of air flow twisting device (1), air is twisted by twisted groove in the inner hollow of air flow twisting device (1) such that air flowing out of air flow twisting device (1) in the twisted condition. Next, the twisted air will create the mixture of air and fuel uniformly disperse causing the stirred effect which creates the distribution of the mixtures of air and fuel in the combustion chamber (6) are more homogenous, and accordingly the engine performance will be greater.</p>
<p id="p0009" num="0009">It is to be understood that the description above which refers to the drawings according to the present invention, is not limited to this embodiment. The prior description of the invention represents only for illustration and explanation. All variations and modifications such as number of air flow twisting device in the inner hollow of air flow twisting device, groove shaped and material of air flow twisting device selected which can be carry out by the person skilled in the art, are considered in the scope of invention stated in the enclosed claim.</p>
</description><!-- EPO <DP n="4"> -->
<claims id="claims01" lang="en">
<claim id="c-en-01-0001" num="0001">
<claim-text>An air flow twisting device (1) which is to be installed after an air filter (5) in the air inlet system of an internal combustion engine having a combustion chamber (6), the air flow twisting device comprising:
<claim-text>a cylindrical housing body made of material such as metal, polymer or ceramic with cylindrical flanges (3) at both ends and with a cavity inside having a first hollow (a) and a second hollow (b), <b>characterized in that</b> the first hollow (a) has a geometry shape of its inner surface with a twisted groove (4) whereas the second hollow (b) has a cylindrical wall without any grooves and <b>in that</b> the first hollow (a) extends over two thirds and the second hollow (b) over one third of the length of the cavity in the housing body of the air flow twisting device (1).</claim-text></claim-text></claim>
</claims><!-- EPO <DP n="5"> -->
<claims id="claims02" lang="de">
<claim id="c-de-01-0001" num="0001">
<claim-text>Luftdrallerzeugungsvorrichtung (1), die nach einem Luftfilter (5) in dem Lufteinlasssystem einer Brennkraftmaschine mit einer Brennkammer (6) anzuordnen ist, wobei die Luftdrallerzeugungsvorrichtung einen zylindrischen Gehäusekörper aus einem Material wie Metall, Polymer oder Keramik mit zylindrischen Flanschen (3) an beiden Enden und mit einem innenseitigen Hohlraum aufweist, der über eine erste Kammer (a) und eine zweite Kammer (b) verfügt, <b>dadurch gekennzeichnet, dass</b> die erste Kammer (a) in einer geometrischen Gestalt ihrer inneren Oberfläche eine gewundene Vertiefung (4) aufweist, während die zweite Kammer (b) über eine zylindrische Wand ohne irgendwelche Vertiefungen verfügt, und dass sich die erste Kammer (a) über zwei Drittel und die zweite Kammer (b) über ein Drittel der Länge des Hohlraums in dem Gehäusekörper der Luftdrallerzeugungsvorrichtung (1) erstrecken.</claim-text></claim>
</claims><!-- EPO <DP n="6"> -->
<claims id="claims03" lang="fr">
<claim id="c-fr-01-0001" num="0001">
<claim-text>Dispositif à flux aéraulique hélicoïdal à monter en aval d'un filtre à air (5) dans le système d'entrée d'air d'un moteur à combustion interne à chambre de combustion (6), le dispositif à flux aéraulique hélicoïdal comprenant :
<claim-text>un corps cylindrique de logement réalisé en une matière telle que du métal, un polymère, une céramique, avec des brides cylindriques (3) à chacune des deux extrémités et une cavité intérieure présentant un premier volume creux (a) et un second volume creux (b), <b>caractérisé en ce que</b> la forme géométrique du premier volume creux (a) présente une surface intérieure à deux gorges hélicoïdales (4) alors que le second volume creux (b) présente une paroi cylindrique sans aucune gorges et <b>en ce que</b> le premier volume creux (a) s'étend sur les deux tiers et le second volume creux sur un tiers de la longueur de la cavité dans le corps de logement du dispositif à flux aéraulique hélicoïdal.</claim-text></claim-text></claim>
</claims><!-- EPO <DP n="7"> -->
<drawings id="draw" lang="en">
<figure id="f0001" num=""><img id="if0001" file="imgf0001.tif" wi="185" he="207" img-content="drawing" img-format="tif"/></figure><!-- EPO <DP n="8"> -->
<figure id="f0002" num=""><img id="if0002" file="imgf0002.tif" wi="172" he="80" img-content="drawing" img-format="tif"/></figure>
</drawings>
</ep-patent-document>
